CN205270625U - Engine pipe pipe end extrusion connecting device - Google Patents

Engine pipe pipe end extrusion connecting device Download PDF

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Publication number
CN205270625U
CN205270625U CN201520950887.0U CN201520950887U CN205270625U CN 205270625 U CN205270625 U CN 205270625U CN 201520950887 U CN201520950887 U CN 201520950887U CN 205270625 U CN205270625 U CN 205270625U
Authority
CN
China
Prior art keywords
lobe
pipe
drift
pipe end
dops
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201520950887.0U
Other languages
Chinese (zh)
Inventor
冯大娟
马艳玲
潘宝山
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AECC Shenyang Liming Aero Engine Co Ltd
Original Assignee
Shenyang Liming Aero Engine Group Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201520950887.0U priority Critical patent/CN205270625U/en
Application granted granted Critical
Publication of CN205270625U publication Critical patent/CN205270625U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an engine pipe pipe end extrusion connecting device, coupling pass through engine pipe pipe end extrusion connecting device and link to each other with the pipe, engine pipe pipe end extrusion connecting device constitutes as follows: drift, three lamella dops, three lamella type heads, clamp splice, clamp splice middle part is provided with half arc recess, and the both sides of half arc recess are provided with the through -hole structure respectively, and the coupling passes through through -hole structure and screw connection in half arc recess of two clamp splices, and the upper end external diameter of three lamella type heads is greater than the external diameter of lower extreme, engine pipe pipe end extrusion connecting device, the external diameter tolerance control that can guarantee the pipe is within 0.2mm, and simple structure is light and handy, low cost, easy operation. Through using the tapering drift to reach labour saving and time saving, have comparatively huge economic value and social value.

Description

A kind of engine duct pipe end extrusion molding coupling device
Technical field
The utility model relates to structure design and the applied technical field of coupling device, specifically provides a kind of engine duct pipe end extrusion molding coupling device.
Background technology
Aircraft engine duct pipe end, the particularly shaping mode of connection of the pipe end of engine thin-walled web member adopt repeatedly shaping, require very high to the level of skill of pincers worker, and labour intensity is big, and Forming Quality is unstable, and rework rate height, therefore the condemnation factor of conduit is approximately 5%. Production efficiency is low, and the work load of workman is big, and the production cycle cannot ensure.
The pipe end of conduit is connected with installation edge forming, and traditional mode of connection adopts 3 cover frocks, and points 3 times shaping, and dismounting inconvenience, Forming Quality instability, working (machining) efficiency is low, and the labour intensity of workman is big.
People urgently wish to obtain the excellent engine duct pipe end extrusion molding coupling device of a kind of technique effect.
Practical novel content
Order of the present utility model is to provide a kind of engine duct pipe end extrusion molding coupling device.
Tube stub is connected with conduit by engine duct pipe end extrusion molding coupling device, and described engine duct pipe end extrusion molding coupling device is constructed as follows: drift 1, three lobe dop 2, three lobe type head 3, fixture block 4, half arc groove 41 it is provided with in the middle part of described fixture block 4, the both sides of half arc groove 41 are respectively arranged with through-hole structure 42, tube stub is connected in half arc groove 41 of two fixture blocks 4 by through-hole structure 42 and screw, the upper end external diameter of three lobe type heads 3 is greater than the external diameter of lower end, three lobe type heads 3 insertion with tube stub pre-assembled after conduit cavity, the upper end external diameter of three lobe dops 2 is greater than the external diameter of lower end, the inner chamber entirety of three lobe dops 2 is in taper, three lobe dops 2 insert in three lobe type heads 3, the lower end of drift 1 is cone structure 11, the middle part of drift 1 is provided with groove structure 12, the cone structure 11 of drift 1 time end inserts the inner chamber of three lobe dops 2, drift 1 and three lobe dops 2 are locked by groove structure 12.
Described engine duct pipe end extrusion molding coupling device, is connected with tube stub cold moulding is extruded for solving conduit. During use, tube stub and conduit pre-assembled, with bolt by fixture block 4 gripping tube fitting, three lobe type heads 3 insert the conduit cavity after pre-assembled, then three lobe dops 2 insert three lobe type head 3 inner chambers, and during work, drift 1 inserts three lobe dop 2 inner chambers. The mode of punching press is taked to realize cold moulding squeeze flow. By tapering drift 1 punching press three lobe dop 2 repeatedly, utilize tapering drift 1 to push ahead in three lobe dops 2 slowly and evenly, thus it is beneficial to the conical surface and reduces the gap between three lobe type head 3 appearance profiles and tube wall, thus realize radial cold moulding extruding.
Pipe wall material embeds in the annular recesses of tube stub inwall, conduit viscous deformation is bigger, tube stub mainly occurs elasticity to be out of shape, after unloading, conduit, tube stub have resilience, but tube stub resilience is relatively big, thus makes conduit together with tube stub compact siro spinning technology, and the cold moulding finally realizing pipe end is extruded. The cold moulding that this device can realize conduit and tube stub is extruded, saves starting material, makes shaping to decrease twice dismounting, twice assembling, reduce frock cost, shortens the process-cycle, greatly improve working (machining) efficiency.
Described engine duct pipe end extrusion molding coupling device, not only can alleviate the labour intensity of workman, and can guarantee junction quality, greatly alleviate work load after application, reduce production cost, it is achieved conduit pipe end is formed connected to be connect.
Described engine duct pipe end extrusion molding coupling device, it is ensured that the outer diameter tolerance of conduit controls within 0.2mm, and the consistence of size can control within 0.1mm. Shaping dimensional precision and consistence all can meet service requirements. Structure is simply light and handy, with low cost, simple to operate. Reach time saving and energy saving with the use of tapering drift, there is comparatively huge economic worth and social value.
Accompanying drawing explanation
Fig. 1 is engine duct pipe end extrusion molding coupling device structural representation;
Fig. 2 is fixture block front view;
Fig. 3 is fixture block vertical view;
Fig. 4 is three lobe dop schematic diagram;
Fig. 5 is drift schematic diagram.
Embodiment
Embodiment 1
Tube stub is connected with conduit by engine duct pipe end extrusion molding coupling device, and described engine duct pipe end extrusion molding coupling device is constructed as follows: drift 1, three lobe dop 2, three lobe type head 3, fixture block 4, half arc groove 41 it is provided with in the middle part of described fixture block 4, the both sides of half arc groove 41 are respectively arranged with through-hole structure 42, tube stub is connected in half arc groove 41 of two fixture blocks 4 by through-hole structure 42 and screw, the upper end external diameter of three lobe type heads 3 is greater than the external diameter of lower end, three lobe type heads 3 insertion with tube stub pre-assembled after conduit cavity, the upper end external diameter of three lobe dops 2 is greater than the external diameter of lower end, the inner chamber entirety of three lobe dops 2 is in taper, three lobe dops 2 insert in three lobe type heads 3, the lower end of drift 1 is cone structure 11, the middle part of drift 1 is provided with groove structure 12, the cone structure 11 of drift 1 time end inserts the inner chamber of three lobe dops 2, drift 1 and three lobe dops 2 are locked by groove structure 12.
Described engine duct pipe end extrusion molding coupling device, is connected with tube stub cold moulding is extruded for solving conduit. During use, tube stub and conduit pre-assembled, with bolt by fixture block 4 gripping tube fitting, three lobe type heads 3 insert the conduit cavity after pre-assembled, then three lobe dops 2 insert three lobe type head 3 inner chambers, and during work, drift 1 inserts three lobe dop 2 inner chambers. The mode of punching press is taked to realize cold moulding squeeze flow. By tapering drift 1 punching press three lobe dop 2 repeatedly, utilize tapering drift 1 to push ahead in three lobe dops 2 slowly and evenly, thus it is beneficial to the conical surface and reduces the gap between three lobe type head 3 appearance profiles and tube wall, thus realize radial cold moulding extruding.
Pipe wall material embeds in the annular recesses of tube stub inwall, conduit viscous deformation is bigger, tube stub mainly occurs elasticity to be out of shape, after unloading, conduit, tube stub have resilience, but tube stub resilience is relatively big, thus makes conduit together with tube stub compact siro spinning technology, and the cold moulding finally realizing pipe end is extruded. The cold moulding that this device can realize conduit and tube stub is extruded, saves starting material, makes shaping to decrease twice dismounting, twice assembling, reduce frock cost, shortens the process-cycle, greatly improve working (machining) efficiency.
Described engine duct pipe end extrusion molding coupling device, not only can alleviate the labour intensity of workman, and can guarantee junction quality, greatly alleviate work load after application, reduce production cost, it is achieved conduit pipe end is formed connected to be connect.
Described engine duct pipe end extrusion molding coupling device, it is ensured that the outer diameter tolerance of conduit controls within 0.2mm, and the consistence of size can control within 0.1mm. Shaping dimensional precision and consistence all can meet service requirements. Structure is simply light and handy, with low cost, simple to operate. Reach time saving and energy saving with the use of tapering drift, there is comparatively huge economic worth and social value.

Claims (1)

1. an engine duct pipe end extrusion molding coupling device, it is characterized in that: tube stub is connected with conduit by engine duct pipe end extrusion molding coupling device, and described engine duct pipe end extrusion molding coupling device is constructed as follows: drift (1), three lobe dops (2), three lobes type head (3), fixture block (4), described fixture block (4) middle part is provided with half arc groove (41), the both sides of half arc groove (41) are respectively arranged with through-hole structure (42), tube stub is connected in half arc groove (41) of two fixture blocks (4) by through-hole structure (42) and screw, the upper end external diameter of three lobes type head (3) is greater than the external diameter of lower end, three lobes type head (3) insertion with tube stub pre-assembled after conduit cavity, the upper end external diameter of three lobe dops (2) is greater than the external diameter of lower end, the inner chamber entirety of three lobe dops (2) is in taper, three lobe dops (2) insert in three lobes type head (3), the lower end of drift (1) is cone structure (11), the middle part of drift (1) is provided with groove structure (12), the cone structure (11) of drift (1) lower end inserts the inner chamber of three lobe dops (2), drift (1) and three lobe dops (2) are locked by groove structure (12).
CN201520950887.0U 2015-11-24 2015-11-24 Engine pipe pipe end extrusion connecting device Expired - Fee Related CN205270625U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520950887.0U CN205270625U (en) 2015-11-24 2015-11-24 Engine pipe pipe end extrusion connecting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520950887.0U CN205270625U (en) 2015-11-24 2015-11-24 Engine pipe pipe end extrusion connecting device

Publications (1)

Publication Number Publication Date
CN205270625U true CN205270625U (en) 2016-06-01

Family

ID=56055246

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520950887.0U Expired - Fee Related CN205270625U (en) 2015-11-24 2015-11-24 Engine pipe pipe end extrusion connecting device

Country Status (1)

Country Link
CN (1) CN205270625U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112873125A (en) * 2021-03-12 2021-06-01 安徽昌宁新材料有限公司 Extrusion pliers matched with pipe fitting

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112873125A (en) * 2021-03-12 2021-06-01 安徽昌宁新材料有限公司 Extrusion pliers matched with pipe fitting

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company

Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City

CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160601

Termination date: 20201124